(7)
Install the five bolts (19) and the washers (20).
(8)
Tighten the bolts (19).
(9)
Connect the tee-connector (1) to the union (3).
(10)
TORQUE the pipe end-fitting (2) to between 12.9 and 14.2 m.daN (95.13 and 104.71 lbf.ft).
(11)
Connect the pipe (25) to the union (27).
(12)
TORQUE the pipe end-fitting (26) to between 9.7 and 10.7 m.daN (71.53 and 78.90 lbf.ft).
(13)
Connect the pipe (22) to the check valve 3022GM.
R 1EFF : 001-049, 051-058, 101-101, 1 29-13-14Page 417 1 1 May 01/05 1 1 1CES 1
(14)
TORQUE the pipe end-fitting (23) to between 12.9 and 14.2 m.daN
(95.13 and 104.71 lbf.ft).
(15)
Connect the pipe (29) to the union (31).
(16)
TORQUE the pipe end-fitting (30) to between 7.5 and 8.3 m.daN (55.30 and 61.20 lbf.ft).
(17)
Install the pipe (46) between the tee-connector (44) an the union (48).
(18)
TORQUE the pipe end-fittings (47), (45) to between 7.5 and 8.3 m.daN
(55.30 and 61.20 lbf.ft).
(19)
Connect the bonding jumper (12) to the structural attachment. Install the bolt (10), the washer (11) and the nut (13).
(20)
Tighten the nut (13).
(21)
Seal the connection of the bonding jumper (12) with SEALANTS (Material No. 09-013).
(22)
Apply STRUCTURE PAINTS (Material No. 16-003) (dyed blue) to the sealant.
(23)
Remove the blanking caps from the electrical connectors.
(24)
Make sure that the electrical connectors are clean and in the correct condition.
(25)
Connect the electrical connectors (5),(41),(42),(43) to the receptacles on the manifold (17).
R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
Subtask 29-13-14-560-050-A
A. Preparation of the Replacement Component
(1) Remove the components which are attached to the removed HP manifold as follows:
NOTE : These components are hydraulically attached to the HP manifold
____
with bobbins:
-
the HP filter 3048GM
-
the relief valve 3063GM.
(a) Remove the HP filter 3048GM as follows:
1_ Hold the HP filter 3048GM and remove the bolts (35),(36) and
the washers (37).
2_ Remove the HP filter 3048GM from the manifold (17).
(b)
Remove the relief valve 3063GM (Ref. TASK 29-13-32-000-001).
(c)
Remove the hydraulic pressure transducer 3065GN (Ref. TASK 29-32-11-000-003).
(d)
Remove the system pressure switch 3151GN (Ref. TASK 29-32-12-000-003).
(e)
Remove the flight-control pressure switch 10CE3 (Ref. TASK 27-92-17-000-002).
(f)
Remove the fluid sampling valve 3187GM (Ref. TASK 29-13-34-000-001).
(g)
Remove the check valve 3022GM as follows: 1 Loosen the check valve 3022GM and remove it at the same time
_ with the O-ring (24).
2 Remove and discard the packing (24).
_
(h)
Remove the bobbins (14),(39) from the manifold (17) (Ref. TASK 20-23-21-911-001).
(i)
Install blanking plugs in the open ports of the manifold (17).
(j)
Remove and discard these items from the bobbins:
-
the square section seals (15), (40)
-
the packings (56), (57)
-
the back-up rings (54), (55), (58), (38).
(k)
Put the bobbins (14),(39) into the BAG - PLASTIC to keep them clean.
(l)
Install blanking plugs in the open ports of all of the removed components.
R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 29-13-14Page 419 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(2) Install the removed components onto the replacement manifold (17) as follows:
NOTE : If the replacement manifold (17) has not been installed
____ before, then the threaded inserts (18) and the cylindrical pin
(16) must be installed.
(a)
Remove the blanking plugs from the ports of the manifold (17) and the components.
(b)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the new packings, back-up rings, square-section seals and the threads of the unions.
(c)
Put the two back-up rings (54) in position on the sides of the bobbins (14) without the identification grooves (equipment side).
(d)
Put the two square-section seals (15) in position on the sides of the bobbins (14) without the identification grooves (equipment side).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM HYDRAULIC POWER 液压3(111)
